# N458UP: 1996 Boeing 757-24APF

- Status: Valid registration
- Airframe: [Boeing 757-24APF](https://openairdocs.org/model/boeing-757-24apf) (registry code 1384969, 178 seats)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Serial number: 25479
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 3, 1996
- Certificate issued: October 4, 1996
- Expires: August 31, 2028
- Mode S code: A591A4
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=458UP
- Page: https://openairdocs.org/aircraft/N458UP

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce RB-211 model are included.

## ADs that may apply (OpenAirDocs): 140 in force

### Matched by airframe (Boeing 757-24APF)

None in force.

### Matched by engine (Rolls-Royce RB-211 series)

- [AD 2026-20-11](https://openairdocs.org/ad/2026-20-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Nov 17, 2026
- [AD 2026-18-04](https://openairdocs.org/ad/2026-18-04): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Oct 16, 2026
- [AD 2026-18-52](https://openairdocs.org/ad/2026-18-52): Turbine Engine Oil System · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Sep 21, 2026
- [AD 2026-18-51](https://openairdocs.org/ad/2026-18-51): Turbine Engine Oil System · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Sep 21, 2026
- [AD 2026-10-06](https://openairdocs.org/ad/2026-10-06): Turbine Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jun 12, 2026
- [AD 2025-05-04](https://openairdocs.org/ad/2025-05-04): Engine Drains · Rolls-Royce Deutschland RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Apr 1, 2025
- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2024-07-04](https://openairdocs.org/ad/2024-07-04): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-524H-36 and RB211-524H-T-36. Effective Apr 15, 2024
- [AD 2023-23-13](https://openairdocs.org/ad/2023-23-13): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 4, 2024
- [AD 2023-22-01](https://openairdocs.org/ad/2023-22-01): Turbine Section · Rolls-Royce Deutschland RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 5 more. Effective Dec 26, 2023
- [AD 2023-21-03](https://openairdocs.org/ad/2023-21-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 5 more. Effective Dec 11, 2023
- [AD 2023-18-05](https://openairdocs.org/ad/2023-18-05): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535C-37. Effective Oct 30, 2023
- [AD 2023-18-01](https://openairdocs.org/ad/2023-18-01): Engine Fuel Pump · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Oct 30, 2023
- [AD 2023-17-12](https://openairdocs.org/ad/2023-17-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Oct 26, 2023
- [AD 2022-09-10](https://openairdocs.org/ad/2022-09-10): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jun 23, 2022
- [AD 2021-08-01](https://openairdocs.org/ad/2021-08-01): Turbine Engine Combustion Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Apr 30, 2021
- [AD 2020-25-04](https://openairdocs.org/ad/2020-25-04): Engine Fireseals · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 8, 2021
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2019-11-07](https://openairdocs.org/ad/2019-11-07): Turbine Engine Compressor Section · Rolls-Royce RB211-524G3-19, RB211-524G3-T-19, RB211-524H-36 and 3 more. Effective Jun 28, 2019
- [AD 2018-18-15](https://openairdocs.org/ad/2018-18-15): Turbine Engine Compressor Section · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Nov 1, 2018
- [AD 2018-18-06](https://openairdocs.org/ad/2018-18-06): Turbine Section · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Sep 20, 2018
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2017-19-16](https://openairdocs.org/ad/2017-19-16): Turbine Engine Compressor Section · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Oct 13, 2017
- [AD 2017-10-13](https://openairdocs.org/ad/2017-10-13): Low-pressure (LP) fuel return tube · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jul 10, 2017
- [AD 2017-10-06](https://openairdocs.org/ad/2017-10-06): Turbine Engine Compressor Section · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jun 9, 2017
- [AD 2017-08-11](https://openairdocs.org/ad/2017-08-11): Engine · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective May 30, 2017
- [AD 2017-08-10](https://openairdocs.org/ad/2017-08-10): Engine · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective May 9, 2017
- [AD 2017-03-03](https://openairdocs.org/ad/2017-03-03): Engine Oil Cooler · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Mar 17, 2017
- [AD 2016-25-10](https://openairdocs.org/ad/2016-25-10): High-pressure compressor (HPC) · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 20, 2017
- [AD 2016-08-07](https://openairdocs.org/ad/2016-08-07): LPT support roller bearing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 22 more. Effective May 16, 2016
- [AD 2016-04-13](https://openairdocs.org/ad/2016-04-13): Sealing sleeve · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Apr 19, 2016
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2015-16-03](https://openairdocs.org/ad/2015-16-03): High-pressure turbine (HPT) blades · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 6 more. Effective Sep 15, 2015
- [AD 2015-07-01](https://openairdocs.org/ad/2015-07-01): Low-pressure turbine (LPT) stage 3 turbine blades · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 4 more. Effective May 8, 2015
- [AD 2015-04-06](https://openairdocs.org/ad/2015-04-06): Electronic engine control (EEC) · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Apr 8, 2015
- [AD 2015-02-20](https://openairdocs.org/ad/2015-02-20): Intermediate-pressure compressor (IPC) rotor shaft · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 22 more. Effective Mar 11, 2015
- [AD 2014-14-01](https://openairdocs.org/ad/2014-14-01): Electronic engine control (EEC) · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Aug 15, 2014
- [AD 2014-13-02](https://openairdocs.org/ad/2014-13-02): LP turbine bearing support and exhaust case assembly · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Aug 5, 2014
- [AD 2014-13-03](https://openairdocs.org/ad/2014-13-03): Electronic engine control (EEC) software · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Jul 14, 2014
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-23-12](https://openairdocs.org/ad/2013-23-12): Low-pressure (LP) compressor fan blade set · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Dec 11, 2013
- [AD 2013-19-21](https://openairdocs.org/ad/2013-19-21): Cracks in the HP compressor stage 1 and 2 disc posts · Rolls-Royce RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36 and 19 more. Effective Nov 6, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2013-05-04](https://openairdocs.org/ad/2013-05-04): Piston ring · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Apr 30, 2013
- [AD 2013-04-01](https://openairdocs.org/ad/2013-04-01): Thrust reverser units (TRUs) · Rolls-Royce RB211-524D4-19, RB211-524D4-39, RB211-524D4-B-19 and 11 more. Effective Mar 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2013-02-03](https://openairdocs.org/ad/2013-02-03): Fuel oil heat exchanger (FOHE) · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Jan 24, 2013
- [AD 2012-25-08](https://openairdocs.org/ad/2012-25-08): High pressure/ intermediate pressure (HP/IP) turbine bearing support oil feed tube outer heat shield · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jan 10, 2013
- [AD 2012-24-05](https://openairdocs.org/ad/2012-24-05): Oil transfer tube · Rolls-Royce RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Dec 26, 2012
- [AD 2012-18-07](https://openairdocs.org/ad/2012-18-07): Low-pressure (LP) compressor blades · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Oct 29, 2012

### Historical (superseded or no longer in force)

- [AD 2021-26-11](https://openairdocs.org/ad/2021-26-11) (historical): Engine Fuel Pump · Rolls-Royce Deutschland RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 3, 2022
- [AD 2020-24-08](https://openairdocs.org/ad/2020-24-08) (historical): Turbine Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jan 4, 2021
- [AD 2020-15-07](https://openairdocs.org/ad/2020-15-07) (historical): Turbine Section · Rolls-Royce Deutschland RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 5 more. Effective Aug 4, 2020
- [AD 2020-06-16](https://openairdocs.org/ad/2020-06-16) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective May 5, 2020
- [AD 2019-05-02](https://openairdocs.org/ad/2019-05-02) (historical): Powerplant/Engine Drains · Rolls-Royce RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Mar 27, 2019
- [AD 2017-22-13](https://openairdocs.org/ad/2017-22-13) (historical): Powerplant/Engine Drains · Rolls-Royce RB211-TRENT 970-84 and RB211-TRENT 972-84. Effective Nov 22, 2017
- [AD 2017-03-02](https://openairdocs.org/ad/2017-03-02) (historical): LP compressor blade · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Mar 22, 2017
- [AD 2017-01-01](https://openairdocs.org/ad/2017-01-01) (historical): Engine (Turbine/Turboprop) · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Jan 26, 2017
- [AD 2016-24-08](https://openairdocs.org/ad/2016-24-08) (historical): Upper bifurcation fairing · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Jan 5, 2017
- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2015-17-19](https://openairdocs.org/ad/2015-17-19) (historical): Fan case low-pressure (LP) fuel tube · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Oct 20, 2015
- [AD 2015-04-03](https://openairdocs.org/ad/2015-04-03) (historical): High- pressure/intermediate-pressure (HP/IP) turbine support internal oil feed tube · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Mar 30, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2014-16-10](https://openairdocs.org/ad/2014-16-10) (historical): LP compressor blades · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Sep 23, 2014
- [AD 2014-05-25](https://openairdocs.org/ad/2014-05-25) (historical): Low-pressure turbine exhaust case and support assembly or tail bearing housing · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Apr 7, 2014
- [AD 2013-26-10](https://openairdocs.org/ad/2013-26-10) (historical): High-pressure (HP) compressor rotor stage 1 and stage 2 discs · Rolls-Royce RB211-524G2-19, RB211-524G3-19, RB211-524H-36 and 1 more. Effective Jan 23, 2014
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2013-15-10](https://openairdocs.org/ad/2013-15-10) (historical): Cracking on the IP compressor rotor shaft rear balance land · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 22 more. Effective Oct 8, 2013
- [AD 2013-12-01](https://openairdocs.org/ad/2013-12-01) (historical): LP compressor blades · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Jul 29, 2013
- [AD 2013-05-18](https://openairdocs.org/ad/2013-05-18) (historical): Fuel tubes and fuel tube clips · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Apr 5, 2013
- [AD 2013-02-04](https://openairdocs.org/ad/2013-02-04) (historical): Low-pressure turbine (LPT) stage 2 disk interstage seal material loss and increased low-pressure rotor vibration while in flight · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Feb 14, 2013
- [AD 2012-10-12](https://openairdocs.org/ad/2012-10-12) (historical): Compressor rotor shafts · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 15 more. Effective Jun 29, 2012
- [AD 2012-06-23](https://openairdocs.org/ad/2012-06-23) (historical): LP compressor blades · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Apr 20, 2012
- [AD 2012-04-13](https://openairdocs.org/ad/2012-04-13) (historical): HP compressor stage 1 and 2 disc posts · Rolls-Royce RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36 and 19 more. Effective Apr 11, 2012
- [AD 2012-04-01](https://openairdocs.org/ad/2012-04-01) (historical): Critical engine parts · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more. Effective Mar 28, 2012
- [AD 2012-02-04](https://openairdocs.org/ad/2012-02-04) (historical): Engine fuel leaks · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Feb 24, 2012
- [AD 2011-13-01](https://openairdocs.org/ad/2011-13-01) (historical): Rivets · Rolls-Royce RB211-524D4-19, RB211-524D4-39, RB211-524D4-B-19 and 11 more. Effective Aug 12, 2011
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2011-09-07](https://openairdocs.org/ad/2011-09-07) (historical): High-pressure compressor (HPC) Stage 1 and 2 disc posts · Rolls-Royce RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36 and 19 more. Effective Jun 7, 2011
- [AD 2011-08-07](https://openairdocs.org/ad/2011-08-07) (historical): LP compressor blades · Rolls-Royce RB211-Trent 884B-17, RB211-Trent 892B-17, RB211-Trent 895-17 and 4 more. Effective Jun 7, 2011
- [AD 2010-16-07](https://openairdocs.org/ad/2010-16-07) (historical): IP turbine · Rolls-Royce RB211-TRENT 970-84, RB211-TRENT 970B-84, RB211-TRENT 972-84 and 4 more. Effective Sep 17, 2010
- [AD 2009-24-05](https://openairdocs.org/ad/2009-24-05) (historical): Fuel pipes · Rolls-Royce RB211-Trent-884B-17, RB211-Trent-892B-17, RB211-Trent-895-17 and 4 more. Effective Jan 4, 2010
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [AD 2008-18-08](https://openairdocs.org/ad/2008-18-08) (historical): IP Compressor rotor · Rolls-Royce RB211-Trent 884B-17, RB211-Trent 892B-17, RB211-Trent 895-17 and 14 more. Effective Oct 14, 2008
- [AD 2007-19-10](https://openairdocs.org/ad/2007-19-10) (historical): Intermediate Pressure Compressor (IP Compressor) Drums · Rolls-Royce RB211 Trent 553-61, RB211 Trent 553A2-61, RB211 Trent 556-61 and 5 more. Effective Oct 3, 2007
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2007-02-05](https://openairdocs.org/ad/2007-02-05) (historical): High pressure-and-intermediate pressure (HP-IP) turbine internal and external oil 
vent tubes · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Feb 6, 2007
- [AD 2006-23-11](https://openairdocs.org/ad/2006-23-11) (historical): High pressure (HP)/intermediate pressure (IP) turbine bearing oil feed tube 
heat shield · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Dec 19, 2006
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2006-05-03](https://openairdocs.org/ad/2006-05-03) (historical): High pressure-intermediate pressure (HP- IP) turbine · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Mar 27, 2006
- [AD 2005-15-13](https://openairdocs.org/ad/2005-15-13) (historical): Intermediate pressure (IP) compressor stage 5 disks · Rolls-Royce RB211-524 Series (all). Effective Aug 30, 2005
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-05](https://openairdocs.org/ad/2004-26-05) (historical): Head section and meterpanel assembly of the combustion liner · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 20 more. Effective Feb 9, 2005
- [AD 2005-01-15](https://openairdocs.org/ad/2005-01-15) (historical): Fan blade dovetail roots · Rolls-Royce RB211-Trent-844B-17, RB211-Trent-884B-17, RB211-Trent-892B-17 and 5 more. Effective Jan 28, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-23-03](https://openairdocs.org/ad/2004-23-03) (historical): High pressure-and-intermediate pressure (HP-IP) turbine internal and external oil vent tubes shaft · Rolls-Royce RB211 Trent 768-60, RB211 Trent 772-60 and RB211 Trent 772B-60. Effective Nov 23, 2004
- [AD 2004-15-02](https://openairdocs.org/ad/2004-15-02) (historical): LP Compressor Fan Blade · Rolls-Royce RB211-Trent-884B-17, RB211-Trent-892B-17, RB211-Trent-895-17 and 4 more. Effective Sep 1, 2004
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003

All 211: https://openairdocs.org/aircraft/N458UP/ads.md

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N458UP.

## FAA accident and incident reports

None matched to N458UP.

## Service difficulty reports (215, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IPXA2026091821733](https://openairdocs.org/sdr/IPXA2026091821733), Sep 18, 2026: EVAS UNIT. UNSECURE. DURING PREFLIGHT FOUND EVAS CONTAINER NOT SECURED/HANGING TO THE SIDE. PLACED CAPT EVAS UNIT ON DEFERRAL IAW MEL 25-60-1. DMP C/W (UNIT REMOVED SERVICEABLE AND 
- [SDR IPXA2026022092281](https://openairdocs.org/sdr/IPXA2026022092281), Feb 2, 2026: SEAT TRACK. CORRODED. STR--UPON VERIFICATION OF REMOVAD FROZEN BOLT AT FWD SIDE OF SEAT TRACK SECTION IN MAIN CABIN STA 880 LBL 20 FOUND CORROSION--ATA 53 MARKED 007-02 REMOVED DAMAG
- [SDR IPXA2026012743275](https://openairdocs.org/sdr/IPXA2026012743275), Jan 23, 2026: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT ANGLE AT APPROX STA 1715 OUTBOARD L/H SIDE, IS CORRODED JUST FWD OF AFT PRESSURE BULKHEAD. DOT AA023. STR ATA 51-00 REMOVED DAMAGED FLOOR SUPPORT 
- [SDR IPXA2026012343275](https://openairdocs.org/sdr/IPXA2026012343275), Jan 23, 2026: FLOOR SUPPORT. CORRODED. AGING ACFT INSP - FLOOR SUPPORT ANGLE AT APPROX STA 1715 OUTBOARD L/H SIDE, IS CORRODED JUST FWD OF AFT PRESSURE BULKHEAD. DOT AA023. STR ATA 51-00
- [SDR IPXA2026022401372](https://openairdocs.org/sdr/IPXA2026022401372), Jan 21, 2026: ANGLE. CORRODED. STR, ATA 55: R/H HORZ STAB TO ELEVATOR MOST OTBD HINGE BONDING STRAPS ATTACH BRACKETS BLOW OUT WITH CORROSION AND BOTH BONDING STRAPS (2 EACH) FRAYED AND CORROD
- [SDR IPXA2026022402462](https://openairdocs.org/sdr/IPXA2026022402462), Jan 21, 2026: ANGLE. CORRODED. LEFT HORZ STAB TO ELEVATOR MOST OTBD HINGE BONDING STRAPS ATTACH BRACKETS HAVE CORROSION AND BOTH BONDING STRAPS (2 EACH) FRAYED AND CORRODED. RL029 INSTALLED 1
- [SDR IPXA2026022323794](https://openairdocs.org/sdr/IPXA2026022323794), Jan 15, 2026: STRAP. CORRODED. CORROSION FOUND ON APU INLET SURROUND STRUCTURE FWD STRAP O/B END . ATA 53 ,STR INSTALLED 4EA STRAP ANGLES AT APU INLET SURROUND STRUCTURE FWD IAW B757-200PF-SR
- [SDR IPXA2025090211532](https://openairdocs.org/sdr/IPXA2025090211532), Aug 28, 2025: HOSE. FAILED. LEFT HYD QTY ANNUNCIATED ON FINAL APPROACH. S HORTLY AFTER LT SYS PRESSURE WAS LOST, AFTER GO AROUND ACCOMPLISHED, QRH PROCEDURE AND RETURNED FOR LANDING. QTY D
- [SDR IPXA2025082811532](https://openairdocs.org/sdr/IPXA2025082811532), Aug 28, 2025: HYDRAULIC SYSTEM. LEAKING. EMERGENCY DECLARED, LT HYD QTY (EICAS C) ANNUNCIATED ON FINAL APPROACH. SHORTLY AFTER LEFT SYSTEM PRESSURE WAS LOST, AFTER GO AROUND ACCOMPLISHED QRH PROCEDURE 
- [SDR IPXA2025082287433](https://openairdocs.org/sdr/IPXA2025082287433), Aug 21, 2025: FLAP SYSTEM. MALFUNCTIONED. EMERGENCY DECLARED ON APPROACH, WHEN CONFIG., TE FLAP DISAGREE EICAS MSG. FLAPS @ BETWEEN 0 AND 1 REMOVED AND REPLACED RT FLAP TRANSMITTER PER AMM 27-58-03/401.
- [SDR IPXA2025062483756](https://openairdocs.org/sdr/IPXA2025062483756), Jun 24, 2025: DOOR. BINDING. CREW ENTRY DOOR DIFFICUILT TO UNLOCK PERFORMED ADJUSTMENT OF CREW ENTRY DOOR IAW AMM 52-12-00, OPS CHECK GOOD AT THIS TIME.
- [SDR IPXA2025062552431](https://openairdocs.org/sdr/IPXA2025062552431), Jun 11, 2025: ATTACH BRACKET. DEBONDED. F/O'S ESCAPE ROPE DOOR ATTACH BRACKETS DISBONDED FROM PANEL, PANEL IS LOOSE. REPLACED F/O'S EMERGENCY ESCAPE ROPE DOOR REFERENCE IPC 25-14-01-02, ITEM 850 & 705
- [SDR IPXA2025061152431](https://openairdocs.org/sdr/IPXA2025061152431), Jun 11, 2025: ATTACH BRACKET. DEBONDED. F/O'S ESCAPE ROPE DOOR ATTACH BRACKETS DISBONDED FROM PANEL, PANEL IS LOOSE DEFERRED F/OS ESCAPE ROPE DOOR PANEL IAW SREO-84962-REQ001 ACOMPLISHED STEPS TO REMO
- [SDR IPXA2025042864245](https://openairdocs.org/sdr/IPXA2025042864245), Apr 26, 2025: LIFE VEST. MISSING. FO'S LIFE JACKET MISSING. REPLACED FO'S LIFE JACKET IAW AMM 25-64-00/201
- [SDR IPXA2024021912973](https://openairdocs.org/sdr/IPXA2024021912973), Feb 5, 2024: TEE ANGLE. CORRODED. FAULT: AFT FUSELAGE, WING TO BODY FAIRING T CHORD SUPPORT AT STA 1220 L/H HAS CORROSION. INSTALLED NEW T-CHORD AT STA 1220 L/H IAW SRM 51-40-02-0G-0. JOB COMPLE
- [SDR IPXA2024021805797](https://openairdocs.org/sdr/IPXA2024021805797), Feb 4, 2024: TEE ANGLE. CORRODED. FAULT: AFT FUSELAGE WTB FAIRING T CHORD SUPPOR AT STA 1240 R/H HAS CORROSION INSTALLED T-CORD SUPPORT AT STA 1240 R/H IAW B757-200 SRM 51-70-12-0G-0, FIG 1. AUD
- [SDR IPXA2024022889259](https://openairdocs.org/sdr/IPXA2024022889259), Feb 3, 2024: SUPPORT. CORRODED. FAULT: WING TO BODY T CHORD SUPPORT AT STA 1220 R/H IS CORRODED INSTALLED NEW "T" CHORD AT STA 1220 R/H IAW SRM 52-40-02
- [SDR IPXA2024022092776](https://openairdocs.org/sdr/IPXA2024022092776), Feb 3, 2024: SKIN. CORRODED. NR 1 ENGINE OUTBD PYLON INNER SKIN, FWD OF VENT PANEL HAS EXFOLIATION CORROSION. ALL WORK ACCOMPLISHED PER EO EO-89461-REQ AND VT MAE 757-5450-27-A3512 REV.
- [SDR IPXA2024022292675](https://openairdocs.org/sdr/IPXA2024022292675), Feb 3, 2024: SKIN. CORRODED. *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT- #2 ENGINE OUTBD PYLON, INNER SKIN FWD OF VENT PANEL HAS EXFOLIATION CORROSION. DOT 8-017. WORK ACCOMPLISHED PER UPS EO:
- [SDR IPXA2024022192899](https://openairdocs.org/sdr/IPXA2024022192899), Feb 3, 2024: DOUBLER. CORRODED. MAJOR REPAIR. #2 ENGINE INBD PYLON INNER SKIN UNDER THE CIRCLE PANEL OPENING HAS CORROSION. DOT 8-021. ACCOMPLISHED WORKED PER UPS EO-89493-REQ 1 AND VT MAE EA 
- [SDR IPXA2024021992798](https://openairdocs.org/sdr/IPXA2024021992798), Feb 3, 2024: SKIN. CORRODED. MAJOR REPAIR, NR 1 ENGINE INBD PYLON INNER SKIN, AFT OF THE SQUARE PANEL HAS EXFOLIATION CORROSION. DOT 8-014. VERIFIED WORKED PER UPS EO: EO 89460-REQ 1 AND VT
- [SDR IPXA2024021992675](https://openairdocs.org/sdr/IPXA2024021992675), Feb 3, 2024: SKIN. CORRODED. MAJOR REPAIR, NR 2 ENGINE OUTBD PYLON, INNER SKIN FWD OF VENT PANEL HAS EXFOLIATION CORROSION. DOT 8-017. OK TO APPLY TOP-COAT APPROVED. OPEN
- [SDR IPXA2024021792899](https://openairdocs.org/sdr/IPXA2024021792899), Feb 3, 2024: SKIN. CORRODED. MAJOR REPAIR, NR 2 ENGINE INBD PYLON INNER SKIN UNDER THE CIRCLE PANEL OPENING HAS CORROSION. DOT 8-021. ACCOMPLISH EO-89493-REQ1 AND EA 757-5450-27-A3519. OPEN
- [SDR IPXA2024021789430](https://openairdocs.org/sdr/IPXA2024021789430), Feb 3, 2024: TEE ANGLE. CORRODED. FAULT: WING TO BODY T CHORD SUPPORT STA 1200 R/H HAS CORROSION INSTALLED T CHORD SUPPORT STA 1200 IAW B757-200 SRM 51-40-02 REVIEWED
- [SDR IPXA2024021589259](https://openairdocs.org/sdr/IPXA2024021589259), Feb 3, 2024: SUPPORT. CORRODED. *** SDR FILED OPEN *** FAULT: WING TO BODY T CHORD SUPPORT AT STA 1220 R/H IS CORRODED AUDIT COMPLETE
- [SDR IPXA2024021592776](https://openairdocs.org/sdr/IPXA2024021592776), Feb 3, 2024: SKIN. CORRODED. FAULT- #1 ENGINE OUTBD PYLON INNER SKIN, FWD OF VENT PANEL HAS EXFOLIATION CORROSION. OK TO INSTALL DOUBLER"INSP ONLY"
- [SDR IPXA2024021773507](https://openairdocs.org/sdr/IPXA2024021773507), Feb 2, 2024: FRAME. DENTED. *MAJOR REPAIR* FAULT: DENT FOUND AT AFT CARGO COMPARTMENT FRAME STA 1500 STR 27 R/H WORKED PER PRELIMINARY 1 AND 2 EA 757-5360-27-A3510 REV-. WORKED PER UPS EO:
- [SDR IPXA2024021673097](https://openairdocs.org/sdr/IPXA2024021673097), Feb 2, 2024: FRAME. DENTED. DENT FOUND AT AFT CARGO COMPARTMENT, STA 1300 STR 27 R/H INSTALLED REPAIR PARTS IAW B757 EA#:757-5360-27-A3513 AND INSTALLED TIE DOWN AND ANGLE AT STA:1300 IAW 
- [SDR IPXA2024021960150](https://openairdocs.org/sdr/IPXA2024021960150), Feb 1, 2024: TEE ANGLE. CORRODED. EVIDENCE OF CORROSION BEHIND PANEL 198LR ON FUSELAGE. INSTALLED T CHORD BEHIND PANEL 189 IAW B757-200 SRM 51-40-02. INSTALLED PANEL 198LR IAW B757-200 SRM 51-40
- [SDR IPXA2022101187064](https://openairdocs.org/sdr/IPXA2022101187064), Oct 11, 2022: POWER SUPPLY. INOPERATIVE. BOTH INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP.REMOVED AND REPLACED BATTERY POWER SUPPLY. MM 33-51-07 AND BATTERY CHARGER. MM 33-51-07. OPS CHECKS GOOD. EFF S
- [SDR IPXA2022021478987](https://openairdocs.org/sdr/IPXA2022021478987), Feb 14, 2022: NONE. NONE. INSPECTION TYPE:C-CKAFT CARGO COMPT. HAS EXISTING REPAIR AT STA 1320 I/B OF S-26R.REMOVED EXISTING REPAIR, FABRICATED STRINGER CLIPS AND COLD WORKED HOLES. REPA
- [SDR IPXA2022021579016](https://openairdocs.org/sdr/IPXA2022021579016), Feb 14, 2022: FRAME. NONE. INSPECTION TYPE:SEG1AFT CARGO COMPTG, FOUND EXISTING FRAME REPAIR AT STA 1560 I/B SODE PF S-26LREPAIRED IAW VT MAE EA#757-5360-27-A2811 REV. UPS EO B757-5310-82
- [SDR IPXA2021120976796](https://openairdocs.org/sdr/IPXA2021120976796), Dec 9, 2021: FIRST AID KIT. NONE. INSPECTION TYPE:N/ASEAL BROKEN ON FIRST AID KITREPLACED FIRST AID KIT AS REQ PER GMM 08-02
- [SDR IPXA2020111062217](https://openairdocs.org/sdr/IPXA2020111062217), Nov 7, 2020: GLIDE SLOPE. FAILED. INSPECTION TYPE: NA DIVERSION, NO EMERGENCY DECLARED. AT 400' ON ILS APPROACH RUNWAY 14 JAX THE FOLLOWING OCCURED. AP DISENGAGED FLIGHT DIRECTOR G/S DEVIATION B
- [SDR IPXA2020092260525](https://openairdocs.org/sdr/IPXA2020092260525), Sep 21, 2020: ACTUATOR. SLOW. EMERGENCY DECLARED. GEAR DISAGREE EICAS MSG ON AFTER TAKEOFF WITH GEAR IN UP POSITION. PLACED ON MEL 32-30-1 HGEAR PINS INSTALLED DMP ACCOMPLISHED. PERFORMED GE
- [SDR IPXA2020062435903](https://openairdocs.org/sdr/IPXA2020062435903), Jun 21, 2020: SENSOR. OUT OF ADJUST. INSPECTION TYPE:SV, ATB - AFTER TAKE OFF, AFTER RETRACTION HAD A GEAR DISAGREE LIGHT, THE LANDING GEAR DISAGREE CHECKLIST RETURNED TO DEPARTURE. NO EMERGENCY WA
- [SDR IPXA2020051555278](https://openairdocs.org/sdr/IPXA2020051555278), May 13, 2020: LIGHT. INOPERATIVE. INSPECTION TYPE:N/AEMERGENCY LIGHT HAS FOUR INOP BULBSRELAMPED EMERGENCT LIGHT PER AMM 33-51-01-2 FOUR BULBS
- [SDR IPXA2020033053628](https://openairdocs.org/sdr/IPXA2020033053628), Mar 11, 2020: SLAT. DELAMINATED. INSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
- [SDR IPXA2020033053627](https://openairdocs.org/sdr/IPXA2020033053627), Mar 11, 2020: SLAT. DELAMINATED. INSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
- [SDR IPXA2020032753623](https://openairdocs.org/sdr/IPXA2020032753623), Mar 11, 2020: SLAT. DELAMINATED. INSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
- [SDR IPXA2019061243113](https://openairdocs.org/sdr/IPXA2019061243113), Jun 10, 2019: STRUCTURE. DAMAGED. RUDDER T/E DMG 26.5 INCHES UP FROM BOTTOM EDGE ON THE L/H SIDE 2.0" ALONG AFT EDGE BY 2.0 FWD/AFT.REPAIRED PER EO B757-5540-72844-A.
- [SDR IPXA2019061243112](https://openairdocs.org/sdr/IPXA2019061243112), Jun 10, 2019: STRUCTURE. DAMAGED. RUDDER T/E DMG 76" UP FROM BOTTOM EDGE. REMOVED DMG IS 1 PLY OF GRAPHITE 1.7" FWD/AFT BY 1.5" UP/DOWN LOCATED ON L/H SIDE.REPAIRED PER EO B757-5540-72844-A.
- [SDR IPXA2019050941939](https://openairdocs.org/sdr/IPXA2019050941939), May 9, 2019: HYDRAULIC LINE. NOT REPORTED. INSPECTION TYPE:N/A AIR TURN BACK - LT HYDRAULIC SYSTEM LOSS OF QUANTITY AND PRESSURE. PASSING 8000 FT. LEFT HYD. QTY EICAS FOLLOWED BY L HYD ENG PUMP EICAS AND
- [SDR IPXA2018032827932](https://openairdocs.org/sdr/IPXA2018032827932), Mar 27, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 251XMF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018040328140](https://openairdocs.org/sdr/IPXA2018040328140), Mar 18, 2018: PANEL. DELAMINATED. INSPECTION TYPE: SEG3, WHILE PERFORMING TAP TEST IAW S55-610-100-2, FOUND THREE AREAS OF DELAMINATION ON THE RT VERTICAL STAB LOWER FWD TORQUE BOX PANEL. REMOVE
- [SDR IPXA2018032527805](https://openairdocs.org/sdr/IPXA2018032527805), Mar 18, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 232XEF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032727899](https://openairdocs.org/sdr/IPXA2018032727899), Mar 15, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XFF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032727896](https://openairdocs.org/sdr/IPXA2018032727896), Mar 15, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 232XJF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032727895](https://openairdocs.org/sdr/IPXA2018032727895), Mar 15, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XJF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032827929](https://openairdocs.org/sdr/IPXA2018032827929), Mar 15, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 252XTF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.

All 215: https://openairdocs.org/aircraft/N458UP/reports.md

## STCs that may be installed (OpenAirDocs) (3)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Rolls-Royce RB-211 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-22B-02
- [STC SE00409LA](https://openairdocs.org/stc/SE00409LA): Installation of gas generator fairing thermal insulation blankets. Air New Zealand Limited. Lists RB211-524G2-19
- [STC SE1516CE](https://openairdocs.org/stc/SE1516CE): Modification of lower fuel control box assembly to incorporate vibration isolators. Trans World Airlines Inc. Lists RB211-22B-02

## Related

- Other Boeing 757-24APF aircraft: https://openairdocs.org/model/boeing-757-24apf/aircraft.md
- The Rolls-Royce RB-211 series engine: https://openairdocs.org/engine/rolls-royce-rb-211-series.md

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